Last edited by Arashiramar
Thursday, April 16, 2020 | History

2 edition of Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft found in the catalog.

Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft

E. Richard White

Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

    Subjects:
  • Stalling (Aerodynamics),
  • Spin (Aerodynamics),
  • Leading edges (Aerodynamics)

  • Edition Notes

    StatementE. Richard White ; prepared for Langley Research Center.
    SeriesNASA contractor report -- 3636., NASA contractor report -- NASA CR-3636.
    ContributionsLangley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Kentron International.
    The Physical Object
    Pagination21 p. :
    Number of Pages21
    ID Numbers
    Open LibraryOL18025119M


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Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft by E. Richard White Download PDF EPUB FB2